The objective of this analysis was to determine the total platform impact on an S-3A avionic suite outfitted with 270 V DC switched mode regulators in lieu of standard 115/200V, 400 Hz transformer coupled series regulators and to quantify the resulting impact in terms of changes to aircraft weight, mission performance, fuel usage, reliability, and LCC. (Author)


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    Title :

    Analysis of the Impact of a 270 VDC Power Source on the Avionic Power Supplies in the S-3A Aircraft


    Publication date :

    1978


    Size :

    233 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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